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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in gas turbines, is of

Axial flow type
Centrifugal type
None of the listed here
Radial flow type

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the ratio of the ________ to the blade velocity is called slip factor.

Outlet velocity of flow
Outlet whirl velocity
Inlet velocity of flow
Inlet whirl velocity

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Compressors, Gas Turbines and Jet Engines
A rocket engine uses __________ for the combustion of its fuel.

Compressed atmospheric air
Surrounding air
Its own oxygen
None of these

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

Compressor
All of these
Cooling chamber
Heating chamber

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Compressors, Gas Turbines and Jet Engines
Ram compression in turbojet involves

Increasing speed of incoming air
Reduction of speed of incoming air and conversion of part of it into pressure energy
Lost work
Compression of inlet air

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Compressors, Gas Turbines and Jet Engines
In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

1 bar
64 bar
16 bar
256 bar

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